A trailing edge cap for a blade includes a body configured to mount on at least two differently at least one of sized and shaped blades such that the body at least partially covers an original trailing edge portion of the blade. The body has a body edge portion for forming a new trailing edge portion of the blade when the body is mounted on the blade.
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20. A method comprising:
#5# providing a trailing edge cap for a blade, wherein the trailing edge cap includes a body that includes a body edge portion having a first thickness defined between a higher pressure side of the body edge portion and a lower pressure side of the body edge portion when the body is mounted on the blade; and
mounting the trailing edge cap on the blade such that the trailing edge cap at least partially covers a trailing edge portion of the blade having a second thickness, the first thickness less than the second thickness.
1. A trailing edge cap for a blade, said trailing edge cap comprising a body configured to mount on at least two blades, wherein each of the at least two blades has at least one of a differing size and a differing shape, said body at least partially covers an original trailing edge portion of the blade, said body having a body edge portion for forming a new trailing edge portion of the blade when said body is mounted on the blade, said body edge portion having a first thickness defined between a higher pressure side of said body edge portion and a lower pressure side of said body edge portion when said body is mounted on the blade, and the original trailing edge portion of the blade having a second thickness defined between a higher pressure side of the blade and a lower pressure side of the blade, said first thickness less than the second thickness. #5#
11. A trailing edge cap for a blade, said trailing edge cap comprising a body configured to mount on the blade such that said body at least partially covers an original trailing edge portion of the blade, said body comprising:
#5# a body edge portion for forming a new trailing edge portion of the blade when said body is mounted on the blade, said body edge portion having a first thickness defined between a higher pressure side of said body edge portion and a lower pressure side of said body edge portion when said body is mounted on the blade, the original trailing edge portion of the blade having a second thickness defined between a higher pressure side of the blade and a lower pressure side of the blade, said first thickness less than the second thickness; and
at least one of a body thickness of between about 1 mil and about 100 mils, a modulus of elasticity of between about 0.5 gpa and about 5 gpa, and a polymer.
15. A blade comprising:
#5# a blade body having a leading edge portion and an original trailing edge portion; and
a trailing edge cap mounted on said blade body and at least partially covering said original trailing edge portion, said trailing edge cap comprising:
a trailing edge cap body comprising a body edge portion having a first thickness defined between a higher pressure side of said body edge portion and a lower pressure side of said body edge portion when said trailing edge cap body is mounted on said blade body, said body edge portion forming a new trailing edge portion of said blade body, said original trailing edge portion of said blade body having a second thickness defined between a higher pressure side of said blade body and a lower pressure side of said blade body, said first thickness less than said second thickness; and
at least one of a trailing edge cap body thickness of between about 1 mil and about 100 mils, a modulus of elasticity of between about 0.5 gpa and about 5 gpa, and a polymer.
2. A trailing edge cap in accordance with 3. A trailing edge cap in accordance with 4. A trailing edge cap in accordance with 5. A trailing edge cap in accordance with 6. A trailing edge in accordance with 7. A trailing edge cap in accordance with 8. A trailing edge cap in accordance with 9. A trialing edge cap in accordance with 10. A trailing edge cap in accordance with 12. A trailing edge cap in accordance with 13. A trailing edge cap in accordance with 14. A trailing edge cap in accordance with 16. A blade in accordance with 17. A blade in accordance with 18. A blade in accordance with
19. A blade in accordance with
21. A method in accordance with
mounting a second side of the trailing edge cap on a lower pressure side of the blade, such that the trailing edge cap at least partially covers a trailing edge portion of the blade formed by an intersection between the higher and lower pressure sides.
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This invention relates generally to blades that may be useful as wind turbine rotor blades and to rotors and wind turbines utilizing such blades.
Some known wind turbine rotor blades may generate considerable noise, particularly at higher rotor speeds, which may bother people and/or entities, for example residential communities, located near the wind turbine. As a consequence, authorities with responsibility for granting permission for setting up wind turbines may refuse permission because of the noise levels. For example, in some parts of the world, issuance of permits for wind turbines is based on the environmental noise impact affected or potentially affected by the wind turbine.
One example of noise emitted by known wind turbine rotor blades is noise emitted from trailing edges of the blades because of interaction between boundary layer air and the trailing edge. Generally, greater trailing edge thicknesses generate higher noise levels. However, manufacturing and transporting blades with a reduced trailing edge thickness may be difficult, for example, without damaging the trailing edge. Accordingly, some known blades include a separate trailing edge piece that covers and reduces a thickness of the trailing edge. The separate trailing edge piece can be mounted on the blade after transportation of the blade to a wind turbine. However, some known separate trailing edge pieces may not mount flush with an outer surface of the blade. Accordingly, although the separate trailing edge piece may reduce a thickness of the blade, a seam between the separate trailing edge piece and the outer surface may increase noise emitted because of interaction of boundary layer air with the seam. Some known rotor blades use custom trailing edge pieces designed to fit generally flush to a specific blade shape. However, such custom trailing edge pieces may only fit the specific blade shape they are designed for and therefore may increase an overall cost of a group of wind turbines having differently shaped rotor blades.
In one aspect, a trailing edge cap for a blade includes a body configured to mount on at least two differently at least one of sized and shaped blades such that the body at least partially covers an original trailing edge portion of the blade. The body has a body edge portion for forming a new trailing edge portion of the blade when the body is mounted on the blade.
In another aspect, a trailing edge cap for a blade includes a body configured to mount on the blade such that the body at least partially covers an original trailing edge portion of the blade. The body includes a body edge portion for forming a new trailing edge portion of the blade when the body is mounted on the blade. The body also includes at least one of a thickness of between about 1 mil and about 100 mils, a modulus of elasticity of between about 0.5 GPa and about 5 GPa, and a polymer.
In another aspect, a blade includes a body having a leading edge portion and an original trailing edge portion, and a trailing edge cap mounted on the body. The trailing edge cap at least partially covers the original trailing edge portion. The trailing edge cap includes an edge portion that forms a new trailing edge portion of the body, and at least one of a thickness of between about 1 mil and about 100 mils, a modulus of elasticity of between about 0.5 GPa and about 5 GPa, and a polymer.
In another aspect, a method includes providing a trailing edge cap for a blade, wherein the trailing edge cap comprises at least one of a thickness of between about 1 mil and about 100 mils, a modulus of elasticity of between about 0.5 GPa and about 5 GPa, and a polymer, and mounting the trailing edge cap on the blade such that the trailing edge cap at least partially covers a trailing edge portion of the blade.
Corresponding reference characters indicate corresponding parts throughout the several views of the drawings.
As used herein, the term “blade” is intended to mean anything that provides reactive force when in motion relative to a surrounding fluid. As used herein, the term “edge” is intended to mean a side formed by the intersection of two things (e.g., sides, surfaces, etc.). An “edge”, as used herein, may include a curved surface. As used herein, the term “sweep” refers to an angle of an elastic axis relative to a pitch axis of a blade, where the “elastic axis” refers to a locus of points defining a torsional or bending center at each spanwise section of the blade. As used herein, the term “trailing edge” is intended to mean a side formed by the intersection of a high pressure side and a low pressure side of a blade. As used herein, the term “wind turbine” is intended to mean anything that generates rotational energy from wind energy, and more specifically, converts kinetic energy of wind into mechanical energy. As used herein, the term “wind generator” is intended to mean a wind turbine that generates electrical power from rotational energy generated from wind energy, and more specifically, converts mechanical energy converted from kinetic energy of wind to electrical power. As used herein, the term “windmill” is intended to mean a wind turbine that uses rotational energy generated from wind energy, and more specifically mechanical energy converted from kinetic energy of wind, for a predetermined purpose other than generating electrical power, such as, but not limited to, pumping a fluid and/or grinding a substance.
Referring now to the drawings, and more specifically to
As shown in
Wind generator 12 includes an electrical generator (not shown) mounted on body 16 and operatively connected to rotor 18 for generating electrical power from the rotational energy generated by rotor 18. General operation of the electrical generator to generate electrical power from the rotational energy of rotor 18 is known in the art and therefore will not be described in more detail herein.
In some embodiments, wind turbine 10 may include one or more controllers (not shown) mounted on body 16 and operatively connected to some or all of the components of wind generator 12 for generally controlling operation of wind generator 12 and/or as some or all of the components thereof (whether such components are described and/or illustrated herein). For example, the controller(s) may be used for overall system monitoring and control including, for example, pitch and speed regulation, high-speed shaft and yaw brake application, yaw and pump motor application, and fault monitoring. Alternative distributed or centralized control architectures may be used in some embodiments. In some embodiments, wind generator 12 may include a brake (not shown) mounted on the body 16 for braking rotation of rotor 18 to, for example, reduce the generation of electrical power from the electrical generator. Furthermore, in some embodiments, wind generator 12 may include a yaw drive (not shown) for rotating wind generator 12 about an axis of rotation 26 for changing a yaw of rotor 18, and more specifically for changing a direction faced by rotor 18 to, for example, adjust an angle between the direction faced by rotor 18 and a direction of wind. Moreover, in some embodiments the wind generator 12 may include an anemometer (not shown) for measuring wind speed. The anemometer, in some embodiments, may be operatively connected to the controller(s) for sending measurements to the controller for processing thereof. In some embodiments, wind generator 12 includes a wind vane (not shown) for measuring wind direction. The wind vane, in some embodiments, may be operatively connected to the controller(s) and/or the yaw drive for changing a yaw of rotor 18. In some embodiments, wind generator 12 includes a variable blade pitch drive (not shown) for controlling a pitch of rotor blades 24. The variable blade pitch drive may be operatively connected to the controller(s) for control thereby. In some embodiments, the pitches of blades 24 are individually controlled by the blade pitch drive. General operation of wind turbine 10, and more specifically wind generator 12, is known in the art and therefore will not be described in more detail herein.
Referring now to
Referring now to
Body 52 of trailing edge cap 50 includes a high pressure side 56 and a low pressure side 58. Any of high pressure side 56 and/or low pressure side 58 may be referred to herein as a first and/or a second side. High pressure side 56 is mounted on high pressure side 36 (
In the exemplary embodiment illustrated herein, trailing edge cap 50 generally spans a majority of the length of blade 24. However, cap 50 is not limited to the size, shape, and/or location illustrated herein. Rather, cap 50 may be any size, any shape, and/or be located on any portion of blade 24 at least partially covering original trailing edge portion 46 of blade 24. For example, in some embodiments cap 50 does not span a majority of the length of blade 24. In some embodiments, some or all of cap 50 may cover original trailing edge portion 46 of blade 24 adjacent tip 34 (
An edge (generally designated by 66) of body 52 is formed by an intersection between high pressure side 56 and low pressure side 58. Body 52 at least partially covers trailing edge 42 of blade 24 such that edge 66 forms a new trailing edge of blade 24. In some embodiments, edge 66 includes a generally “pointed” side, as shown in
Body 52 of trailing edge cap 50 may be fabricated in any manner, fashion, way, configuration, and/or by any means. For example, in some embodiments a shape of body 52 is cut from a material using a laser, water, and/or a clicker die. In some embodiments, body 52 is fabricated from a unitary sheet of material that is creased to form edge 66. In some embodiments, body 52 is fabricated from two or more separate sheets of material that are pre-cut and then bonded together using, for example, a suitable adhesive. In some embodiments, such two or more separate sheets of material may be bonded together generally adjacent edge 66 of body 52. For example, the bond between the separate sheets may facilitate forming edge 66.
Body 52 may include any material having one or more of the properties (such as, but not limited to, thickness, modulus of elasticity, etc.) described herein with respect thereto. Although body 52 may include other materials, in some embodiments body 52 includes a polymer. For example, and although body 52 may include other polymers, in some embodiments body 52 includes a polyimide, such as, but not limited to, Dupont Kapton® available from Dupont High Performance Materials of Circleville, Ohio. Moreover, and for example, although body 52 may include other polymers, in some embodiments body 52 includes polyester. Furthermore, and for example, although body 52 may include other polymers, in some embodiments body 52 includes polyester terathalate (PET). Even further, and for example, although body 52 may include other polymers, in some embodiments body 52 includes polyetheretherketone (PEEK).
Although body 52 may have other thicknesses, in some embodiments body 52 includes a thickness t (
Although body 52 may include other values for modulus of elasticity, in some embodiments body 52 includes a modulus of elasticity of between about 0.5 GPa and about 5 GPa. In some embodiments, body 52 includes a modulus of elasticity that is generally uniform throughout body 52. In some embodiments, body 52 does not have a generally uniform modulus of elasticity throughout.
As discussed above, and referring now to
By providing a reduced thickness of a trailing edge portion of blade 24, trailing edge cap 50 reduces an amount of noise emitted by the blade 24 during operation thereof, such as, but not limited to, noise emitted by a trailing edge portion of blade 24. For example, the reduced thickness of edge 66 of trailing edge cap 50 may reduce an amount of separated flow downstream of blade 24 and therefore may reduce, for example, noise sometimes referred to as “blunt trailing edge noise”.
Body 52 of trailing edge cap 50 is configured to be mounted on more than one differently sized and/or shaped blades 24, such as, but not limited to, swept blades, straight blades, twisted blades, etc. For example, because of the thickness, modulus of elasticity, type of material, and/or other properties (whether described herein) of body 52, body 52 has a flexibility that allows body 52 to conform a variety of differently sized and/or shaped trailing edge portions 46 of blades 20, to thereby create a new trailing edge portion of blade 24 from edge portion 54 of cap 50. Moreover, and for example, in addition or alternative to a general flexibility of sides 56 and 58, conformation of cap 50 to a variety of differently sized and/or shaped trailing edge portions 46 of blades 20 may be facilitated by changing an angle between the sides 56 and 58 by bending cap 50 about edge 66 of cap 50. Furthermore, and for example, conformation of cap 50 to a variety of differently sized and/or shaped trailing edge portions 46 of blades 20 may be facilitated by a position of cap 50 with respect to blade 24, such as, but not limited to, an amount that sides 56 and/or 58 overlap sides 36 and/or 38, respectively. The thickness, modulus of elasticity, type of material, and/or other properties (whether described herein) of body 52 may, in some embodiments, be selected to facilitate providing the herein-described flexibility while still maintaining enough strength to facilitate preventing sides 56 and/or 58 from buckling, vibrating, and/or generally deforming under wind loading. In some embodiments, one or more supports (not shown) supports side 56 and/or side 58 to facilitate preventing side 56 and side 58 from buckling, vibrating, and/or generally deforming under wind loadings. For example, in some embodiments foam may be injected between cap 50 and original trailing edge portion 46 of blade 24 to at least partially fill a space defined therebetween for supporting side 56 and/or side 58.
Conformation of cap 50 to a variety of differently sized and/or shaped trailing edge portions 46 of blades 20 may facilitate reducing an overall cost of a group of wind turbines having differently sized and/or shaped blades 24, because custom trailing edge pieces may not be fabricated for each different sized and/or shaped blade 24. Moreover, such conformation to a variety of differently sized and/or shaped trailing edge portions 46 may facilitate increasing and an availability of trailing edge pieces that create new trailing edge portions on blades located at wind turbines. Additionally, the herein-described thicknesses and types of materials of body 52 may facilitate decreasing a cost of blades 24 and/or a weight of blades 24, and/or may facilitate increasing an aerodynamic efficiency of blades 24. Furthermore, the herein described thicknesses of body 52 facilitate reducing a seam created between the body 52 and the blade 24 thereby possibly reducing an amount of noise emitted from blade 24 adjacent and because of the seam.
Embodiments of methods, caps, and blades of the present invention are described and illustrated herein with respect to a wind turbine, and more specifically, a wind generator. However, embodiments (whether described and/or illustrated herein) of the methods, caps, and blades of the present invention are not limited to wind generators, nor wind turbines generally. Rather, embodiments (whether described and/or illustrated herein) of the methods, caps, and blades of the present invention may be applicable to anything having one or more blades.
Exemplary embodiments of the present invention are described and/or illustrated herein in detail. The embodiments are not limited to the specific embodiments described herein, but rather, components and steps of each embodiment may be utilized independently and separately from other components and steps described herein. Each embodiment's components and steps can also be used in combination with other embodiment's (whether described and/or illustrated herein) components and/or steps.
When introducing elements of the embodiments of the present invention, the articles “a”, “an”, “the” and “said” are intended to mean that there are one or more of the elements. The terms “comprising”, “including” and “having” are intended to be inclusive and mean that there may be additional elements other than the listed elements. Moreover, use of the term “portion” with respect to something is intended to some or all of the thing.
While the invention has been described in terms of various specific embodiments, those skilled in the art will recognize that embodiments (whether described and/or illustrated herein) of the present invention can be practiced with modification within the spirit and scope of the claims.
Herr, Stefan, Driver, Howard Daniel
Patent | Priority | Assignee | Title |
10100805, | Oct 12 2015 | GE INFRASTRUCTURE TECHNOLOGY LLC | Tip extension assembly for a wind turbine rotor blade |
10180125, | Apr 20 2015 | GE INFRASTRUCTURE TECHNOLOGY LLC | Airflow configuration for a wind turbine rotor blade |
10337490, | Jun 29 2015 | GE INFRASTRUCTURE TECHNOLOGY LLC | Structural component for a modular rotor blade |
10443579, | Nov 15 2016 | GE INFRASTRUCTURE TECHNOLOGY LLC | Tip extensions for wind turbine rotor blades and methods of installing same |
10465652, | Jan 26 2017 | GE INFRASTRUCTURE TECHNOLOGY LLC | Vortex generators for wind turbine rotor blades having noise-reducing features |
10487796, | Oct 13 2016 | GE INFRASTRUCTURE TECHNOLOGY LLC | Attachment methods for surface features of wind turbine rotor blades |
10746157, | Aug 31 2018 | GE INFRASTRUCTURE TECHNOLOGY LLC | Noise reducer for a wind turbine rotor blade having a cambered serration |
10767623, | Apr 13 2018 | GE INFRASTRUCTURE TECHNOLOGY LLC | Serrated noise reducer for a wind turbine rotor blade |
10773464, | Nov 21 2017 | General Electric Company | Method for manufacturing composite airfoils |
10821652, | Nov 21 2017 | GE INFRASTRUCTURE TECHNOLOGY LLC | Vacuum forming mold assembly and method for creating a vacuum forming mold assembly |
10821696, | Mar 26 2018 | GE INFRASTRUCTURE TECHNOLOGY LLC | Methods for manufacturing flatback airfoils for wind turbine rotor blades |
10830206, | Feb 03 2017 | GE INFRASTRUCTURE TECHNOLOGY LLC | Methods for manufacturing wind turbine rotor blades and components thereof |
10865769, | Nov 21 2017 | General Electric Company | Methods for manufacturing wind turbine rotor blade panels having printed grid structures |
10913216, | Nov 21 2017 | General Electric Company | Methods for manufacturing wind turbine rotor blade panels having printed grid structures |
10920745, | Nov 21 2017 | GE INFRASTRUCTURE TECHNOLOGY LLC | Wind turbine rotor blade components and methods of manufacturing the same |
11035339, | Mar 26 2018 | GE INFRASTRUCTURE TECHNOLOGY LLC | Shear web assembly interconnected with additive manufactured components |
11040503, | Nov 21 2017 | General Electric Company | Apparatus for manufacturing composite airfoils |
11098691, | Feb 03 2017 | General Electric Company | Methods for manufacturing wind turbine rotor blades and components thereof |
11248582, | Nov 21 2017 | General Electric Company | Multiple material combinations for printed reinforcement structures of rotor blades |
11274650, | Oct 13 2016 | GE INFRASTRUCTURE TECHNOLOGY LLC | Attachment methods for surface features of wind turbine rotor blades |
11390013, | Nov 21 2017 | GE INFRASTRUCTURE TECHNOLOGY LLC | Vacuum forming mold assembly and associated methods |
11548246, | Nov 21 2017 | General Electric Company | Apparatus for manufacturing composite airfoils |
11668275, | Nov 21 2017 | General Electric Company | Methods for manufacturing an outer skin of a rotor blade |
7976276, | Nov 04 2010 | GE INFRASTRUCTURE TECHNOLOGY LLC | Noise reducer for rotor blade in wind turbine |
7976283, | Nov 10 2010 | GE INFRASTRUCTURE TECHNOLOGY LLC | Noise reducer for rotor blade in wind turbine |
7988421, | Mar 31 2009 | GE INFRASTRUCTURE TECHNOLOGY LLC | Retrofit sleeve for wind turbine blade |
8038407, | Sep 14 2010 | GE INFRASTRUCTURE TECHNOLOGY LLC | Wind turbine blade with improved trailing edge bond |
8057189, | Dec 15 2010 | GE INFRASTRUCTURE TECHNOLOGY LLC | Wind turbine blade with modular leading edge |
8083488, | Aug 23 2010 | GE INFRASTRUCTURE TECHNOLOGY LLC | Blade extension for rotor blade in wind turbine |
8092187, | Dec 30 2008 | GE INFRASTRUCTURE TECHNOLOGY LLC | Flatback insert for turbine blades |
8182731, | Jan 21 2011 | GE INFRASTRUCTURE TECHNOLOGY LLC | Method of manufacturing a retrofit sleeve for wind turbine blade |
8267657, | Dec 16 2010 | GE INFRASTRUCTURE TECHNOLOGY LLC | Noise reducer for rotor blade in wind turbine |
8297933, | Dec 15 2010 | GE INFRASTRUCTURE TECHNOLOGY LLC | Wind turbine blade with modular leading edge |
8403642, | Sep 27 2011 | GE INFRASTRUCTURE TECHNOLOGY LLC | Wind turbine rotor blade assembly with root curtain |
8414261, | May 31 2011 | GE INFRASTRUCTURE TECHNOLOGY LLC | Noise reducer for rotor blade in wind turbine |
8430638, | Dec 19 2011 | GE INFRASTRUCTURE TECHNOLOGY LLC | Noise reducer for rotor blade in wind turbine |
8506250, | Oct 19 2011 | GE INFRASTRUCTURE TECHNOLOGY LLC | Wind turbine rotor blade with trailing edge extension and method of attachment |
8523515, | Nov 15 2010 | GE INFRASTRUCTURE TECHNOLOGY LLC | Noise reducer for rotor blade in wind turbine |
8834117, | Sep 09 2011 | General Electric Company | Integrated lightning receptor system and trailing edge noise reducer for a wind turbine rotor blade |
8834127, | Sep 09 2011 | GE INFRASTRUCTURE TECHNOLOGY LLC | Extension for rotor blade in wind turbine |
8851855, | Jul 05 2010 | Rolls-Royce plc | Composite turbomachine blade |
8876064, | Dec 21 2009 | RAMOT AT TEL-AVIV UNIVERSITY LTD | Oscillatory vorticity generator and applications thereof |
8878377, | Dec 21 2007 | VESTAS WIND SYSTEMS A S | Wind turbine, a method for reducing noise emission from a wind turbine tower and use of a wind turbine |
9157327, | Feb 26 2010 | RTX CORPORATION | Hybrid metal fan blade |
9297357, | Apr 04 2013 | GE INFRASTRUCTURE TECHNOLOGY LLC | Blade insert for a wind turbine rotor blade |
9458821, | Sep 11 2012 | GE INFRASTRUCTURE TECHNOLOGY LLC | Attachment system for a wind turbine rotor blade accessory |
9494134, | Nov 20 2013 | GE INFRASTRUCTURE TECHNOLOGY LLC | Noise reducing extension plate for rotor blade in wind turbine |
9506452, | Aug 28 2013 | GE INFRASTRUCTURE TECHNOLOGY LLC | Method for installing a shear web insert within a segmented rotor blade assembly |
9556849, | May 02 2013 | GE INFRASTRUCTURE TECHNOLOGY LLC | Attachment system and method for wind turbine vortex generators |
9670902, | Nov 25 2011 | SUZLON ENERGY LIMITED | Blade for a wind turbine having a guide vane |
9677537, | Mar 28 2013 | GE INFRASTRUCTURE TECHNOLOGY LLC | Acoustic shield for noise reduction in wind turbines |
9869295, | May 07 2015 | GE INFRASTRUCTURE TECHNOLOGY LLC | Attachment method to install components, such as tip extensions and winglets, to a wind turbine blade, as well as the wind turbine blade and component |
9869296, | May 07 2015 | GE INFRASTRUCTURE TECHNOLOGY LLC | Attachment method and system to install components, such as tip extensions and winglets, to a wind turbine blade |
9869297, | May 07 2015 | GE INFRASTRUCTURE TECHNOLOGY LLC | Attachment method and system to install components, such as vortex generators, to a wind turbine blade |
9890764, | Mar 26 2014 | GE INFRASTRUCTURE TECHNOLOGY LLC | Trailing edge cap for a rotor blade and method of manufacturing same |
9897065, | Jun 29 2015 | GE INFRASTRUCTURE TECHNOLOGY LLC | Modular wind turbine rotor blades and methods of assembling same |
Patent | Priority | Assignee | Title |
4295790, | Jun 21 1979 | The Budd Company | Blade structure for use in a windmill |
4462559, | Sep 07 1982 | Means for controlling lateral movement of a helicopter | |
5499904, | Jul 12 1993 | FloWind Corporation | Vertical axis wind turbine with pultruded blades |
5533865, | Nov 04 1993 | STORK PRODUCT ENGINEERING B V | Wind turbine |
5542820, | Dec 23 1994 | Sikorsky Aircraft Corporation | Engineered ceramic components for the leading edge of a helicopter rotor blade |
5881972, | Mar 05 1997 | United Technologies Corporation | Electroformed sheath and airfoiled component construction |
6132181, | Jul 31 1995 | Windmill structures and systems | |
6139278, | May 20 1996 | General Electric Company | Poly-component blade for a steam turbine |
6213721, | Nov 09 1993 | THALES HOLDINGS UK PLC | Noise emission reduction |
6253101, | Feb 04 1999 | Siemens Healthcare GmbH | Method for the operation of a diagnostic magnetic resonance apparatus |
6341747, | Oct 28 1999 | United Technologies Corporation | Nanocomposite layered airfoil |
6478541, | Aug 16 2001 | The Boeing Company | Tapered/segmented flaps for rotor blade-vortex interaction (BVI) noise and vibration reduction |
6729846, | Dec 09 1998 | Reduction in the noise produced by a rotor blade of a wind turbine | |
6830436, | Feb 22 2002 | MITSUBISHI HEAVY INDUSTRIES, LTD | Wind turbine provided with nacelle |
20030175121, | |||
20030184292, | |||
20050008495, | |||
20050053466, |
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